| Type | Aircraft | |
| Company | Groupe Latécoère | |
| Scheme | Biplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
16.0
88.7
|
|
| Height (m) |
0.6
4.7
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
120
925
|
|
| Wingspan (Beam) (m) |
0.1
27.7
95
|
|
| Weights | ||
| Empty weight (kg) |
8
5,050
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
7,050
575,000
|
|
| Loaded weight (kg) |
5
6,590
242,500
|
|
| Capacity | ||
| Crew (per.) |
1
4
112
|
|
| Speeds | ||
| Ground Speed (km/h) |
96.6
198
1,500
|
|
| Сruise Speed (km/h) |
52
166
3,087
|
|
| Power | ||
| Total Power (hp) |
0.4
1,680
60,000
|
4 powerplants 420 hp each |
| Performance | ||
| Service ceiling (m) |
0.6
6,500
161,544
|
|
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
246
36,000
|
|
| Combat | ||
| Guns (qt) |
1
3
18
|
7.7 mm (0.303 in) Lewis machine guns in dorsal, ventral and nose positions |
| Stat | ||
| Number built (qt) |
0
1
43,000
|
|
| Introduction | 1924 | |
| First flight | 01.06.1924 | |
